NREL's S832 Airfoil (s832-nr)
NREL's S832 Airfoil - NREL HAWT airfoil S832
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(s832-nr) NREL's S832 Airfoil NREL HAWT airfoil S832 Max thickness 14.9% at 44% chord. Max camber 5.3% at 44% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S832 Airfoil x/c y/c 1.000000 0.000000 0.996189 0.000690 0.985144 0.003330 0.967848 0.008395 0.945387 0.015755 0.918585 0.024881 0.887880 0.035169 0.853519 0.046383 0.816140 0.058387 0.776422 0.070791 0.734962 0.083121 0.692288 0.094860 0.648822 0.105440 0.604799 0.114365 0.560397 0.121287 0.515766 0.125985 0.471058 0.128305 0.426293 0.128244 0.381615 0.126142 0.337467 0.122329 0.294358 0.117013 0.252745 0.110366 0.213098 0.102561 0.175832 0.093763 0.141367 0.084153 0.110065 0.073902 0.082279 0.063197 0.058313 0.052175 0.038300 0.041018 0.022423 0.030004 0.010713 0.019421 0.003282 0.009733 0.000114 0.001503 0.000004 0.000278 0.000099 -0.001261 0.000264 -0.001935 0.000525 -0.002520 0.000941 -0.003030 0.001503 -0.003525 0.001881 -0.003804 0.002983 -0.004482 0.010744 -0.007277 0.025774 -0.009577 0.047344 -0.010877 0.075097 -0.011915 0.108254 -0.012945 0.146278 -0.014035 0.188463 -0.015224 0.234228 -0.016488 0.282871 -0.017793 0.333771 -0.019071 0.386222 -0.020247 0.439587 -0.021223 0.493169 -0.021885 0.546335 -0.022084 0.598428 -0.021585 0.649107 -0.020048 0.698213 -0.017446 0.745551 -0.013944 0.790900 -0.009907 0.833844 -0.005849 0.873785 -0.002344 0.909799 0.000129 0.940887 0.001438 0.966133 0.001687 0.984757 0.001184 0.996164 0.000414 1.000000 0.000000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
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Polars for NREL's S832 Airfoil (s832-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s832-nr | 50,000 | 9 | 19.8 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 50,000 | 5 | 16 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 100,000 | 9 | 26.4 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 100,000 | 5 | 25.2 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 200,000 | 9 | 54.7 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 200,000 | 5 | 67.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 500,000 | 9 | 126 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 500,000 | 5 | 118.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s832-nr | 1,000,000 | 9 | 163.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s832-nr | 1,000,000 | 5 | 151.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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